发明名称 Aircraft body member, more particularly for supersonic aircraft, made from a long-living, damage tolerant aluminium alloy with good stress corrosion resistance
摘要 <p>An aircraft component is made of an Al alloy containing 2.00-3.00 wt.% Cu, 1.40-1.90 wt.% Mg, 0.20-0.70 wt.% Mn, 0-0.30 wt.% Fe, 0-0.30 wt.% Ni, 0-0.15 wt.% Ti, at least 0.05 wt.% Si and 0-1.10% Ag, where 0.40 &le; Si + 0.4 Ag &le; 0.60 and Si + Ag + 1.1 Mg &le; 2.6. One alloy exemplified contains 0.40-0.60% Si and no Ag, and another contains 0.20-0.40% Si and 0.40-0.60% Ag.</p>
申请公布号 EP0756016(A1) 申请公布日期 1997.01.29
申请号 EP19960401680 申请日期 1996.07.26
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 PONS, GILLES;BARBAUX, YANN PHILIPPE
分类号 C22C21/12;C22C21/16;(IPC1-7):C22C21/16 主分类号 C22C21/12
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